Difference between revisions of "T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine/Box"
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− | |part= | + | |filename=liquidEngineAerospike.cfg |
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+ | {{Infobox/Part/test subject | ||
+ | |environments=15 | ||
+ | |staging=True | ||
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Revision as of 01:36, 8 October 2014
T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine | ||
Liquid fuel engine by C7 Aerospace Division | ||
Radial size | Small | |
Cost | (total) | 3 850.00 |
Mass | (total) | 1.500 t |
Drag | 0.2 | |
Max. Temp. | 3600 K | |
Impact Tolerance | 20 m/s | |
Research | Hypersonic Flight | |
Unlock cost | 42 000 | |
Since version | 0.15 | |
Part configuration | liquidEngineAerospike.cfg | |
Maximum thrust | (1 atm) | 174.10 kN |
(vacuum) | 175.00 kN | |
Isp | (1 atm) | 388 s |
(vacuum) | 390 s | |
Fuel consumption | 9.15 /s | |
Thrust vectoring | No | |
Testing Environments | ||
On the surface | Yes | |
In the ocean | Yes | |
On the launchpad | Yes | |
In the atmosphere | Yes | |
Sub-orbital | No | |
In an orbit | No | |
On an escape | No | |
Docked | No | |
Test by staging | Yes | |
Manually testable | Yes |